N436US, cancelled Feb 2, 2007
Service difficulty reports · 42
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N436US' AND deregistration_id = 'N436US-2007-02-02' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N436US' AND deregistration_id = 'N436US-2007-02-02' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA050352Skin · delaminatedPIT - C5 - SLAT, 3 INCH LONG X 2.5 INCH WIDE - 2 AREAS, DELAMINATION. NR 5 SLAT TOP SURFACE IB AND OB T/E. INSTALED NEW CORE, TOP DOUBLERS, SEAL AND REFINISH IAW SRM. (K)SDR USAA050215Cargo Track · crackedPIT - FOUND CARGO FLOOR TIE DOWN CRACKED .125 INCH, FLOOR TIE DOWN RBBL 13.88 STATION 767 IN RADIUS. REMOVED AND REPLACED CARGO FLOOR TIE DOWN TRACK PER SRM 51-40-02. (M)SDR USAA050216Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED 1 INCH, LEFT LEADING EDGE LOWER SKIN PANEL AT SLAT STATION 3.25. FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 57-41-02. (M)SDR USAA050217Clip · corrodedPIT - FOUND CLIP CORRODED 1 INCH BY 3 INCH AREA, FRAME 795, STRINGER 27R. CORROSION LEVEL 1, TASK C53-208-01. CUT OUT DAMAGE AND INSTALLED DOUBLER REPAIR PER EA 79752, SRM 53-00-07 FIG 207. (M)SDR USAA050197Support Fitting · chafedPIT - FOUND SPOILER CHAFED .5 INCH, NR 4 GROUND SPOILER INBOARD SUPPORT FITTING. INSTALLED ANGLE PER TYP REPAIR 57-50-14. (M)SDR USAA050193Web · corrodedPIT - FOUND WEB CRACKED 1 INCH BY 2 INCH AREA AROUND NUT PLATE, AFT CARGO THRESHOLD WEB STATION 800 TO 833 PLATE. CORROSION LEVEL 1. REMOVED WEB AND REPLACED WITH NEW WEB PER SRM 53-60-15, 51-40-02. (M)SDR USAA050196Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 4 INCH BY 8 INCH AREA, AT NUT PLATE HOLES, RT Z-ANGLE AT AFT SERVICE DOOR BS 950-990. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-00. (M)SDR USAA050195Mount · corrodedPIT - FOUND MOUNT GALLEY AFT CORRODED 3 INCH BY 3 INCH AREA, LEFT AFT GALLEY MOUNT BS 990, BS 1016 LBL 32.10. REPLACED MOUNT LEFT AFT GALLEY PER SRM 51-40-00. (M)SDR USAA050204Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 827. CUT OUT DAMAGE, HI FREQ, INSTALLED DOUBLER PER TR 53-10-20A. (M)SDR USAA050203Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, BETWEEN STRINGER 8L AND 9L AT STATION 867. CUT OUT DAMAGED AREA, HI FREQ INSTALLED DOUBLER PER TR 53-10-20A. (M)SDR USAA050200Support Beam · gougedPIT - Q3 - MLG SUPPORT BEAM, .025 DEEP .250 X .125 (4 EA) GOUGE; LT MLG SUPPORT BEAM, LOWER FLANGE AFT EDGE 37 INCHES OB OF IB EDGE. (K)SDR USAA050214Floorbeam · corrodedPIT - FOUND BEAM CORRODED 2 INCH BY 100 INCH AREA, BS 986.5 FLOORBEAM ENTIRE UPPER SURFACE. SPLICED IN NEW UPPER CAP PER TYPICAL REPAIR 53-60-01 REV A. (M)SDR USAA050202Stringer · crackedPIT - FOUND STRINGER CRACKED .25 INCH, STATION 907 STRINGER 4R. DOUBLER INSTALLED PER SRM 53-00-03 FIG 201. (M)SDR USAA050192Intercostal · corrodedPIT - FOUND INTERCOSTAL CORRODED 2 INCH BY 2 INCH AND 4 INCH BY 4 INCH, BS 947 TO 967 LBL 50. CORROSION LEVEL 1, TASK C53-107-102. REPLACED WITH BOEING PART PER SRM 51-40-04. (M)SDR USAA050209Skin Panel · crackedPIT - FOUND SKIN PANEL CRACKED .5 INCH LONG, OUTBOARD SIDE OF PYLON ABOVE MID SPAR FITTING LOWER SKIN PANEL SLAT STATION 3.25. STOP DRILLED, INSTALLED FILLER AND DOUBLER FREEZE PLUG PER TR 57-41-02, SRM 51-20-10 AND EA 79764. (M)SDR USAA050208Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .5 INCH, 2 FASTENER HOLES STATION 500G TO 520 BL 0. INSTALLED INTERCOSTAL PER 53-30-51. (M)SDR USAA050210Frame · crackedPIT - FOUND FRAME CRACKED TWO PLACES .125 INCH LONG, STATION 500A BETWEEN STRINGER 8LT AND 9L OVERHEAD BIN LOWER ATTACH POINT. REINFORCED WITH PREFABRICATED DOUBLERS PER TYPICAL REPAIR 53-10-20A. (M)SDR USAA050213Mount · corrodedPIT - FOUND LAV FLOOR MOUNT CORRODED 2 INCH BY 2 INCH AREA, STATION 304, LBL 12. REPLACED FITTING PER 53-10-00. CORROSION LEVEL 1. (M)SDR USAA050191Floorbeam · corrodedPIT - FOUND UPPER CHORD CORRODED 8 INCH BY 2 INCH, STATION 312 LBL 8 TO RBL 7 FLOOR UPPER CHORD. REPLACED UPPER CHORD PER SRM 53-10-51 FIG 205. (M)SDR USAA050212Structure · crackedPIT - FOUND AFT CARGO DOOR CRACKED .25 INCH, LOWER T-CHORD AFT VERTICAL FLANGE. REMOVED AND REPLACED T-CHORD PER BOEING BLUEPRINT 65-47952. (M)SDR USAA050199Intercostal · burnedPIT - Q3 - INTERCOSTAL UNK SIZE- ARC BURN DAMAGE; GROUND STUD GD 3252, STA 344-360, LBL60 WL 204. REPLACED INTERCOSTAL IAW EA. (K)SDR USAA050211Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED 1.75 INCH, STATION 384-386 IN RADIUS OF INTERCOSTAL BL 0. INSTALLED INTERCOSTAL PER 53-20-1/53-30-1. (M)SDR USAA050206Skin · crackedPIT - FOUND SLAT CRACKED .5 INCH, FORWARD OF INBOARD AUX TRACK LOWER SURFACE AFT FASTENER. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)SDR USAA050205Clip · crackedPIT - FOUND FRAME CLIP CRACKED .5 INCH, STATION 706 S11L. FABRICATED AND INSTALLED NEW CLIP PER SRM 51-46-03 AND 51-70-11. (M)SDR USAA050190Tie Clip · crackedPIT - FOUND STRINGER TIE CLIP CRACKED, .5 INCH IN RADIUS AREA, STRINGER TIE CLIP, STATION 1006, STRINGER 2R. DEFECTIVE PART REPLACED WITH IDENT PART PER TYPICAL REPAIR 57-50-55. (M)SDR USAA040679Bracket · crackedPIT - FOUND BRACKET CRACKED .5 INCH, FORWARD SERVICE DOOR LOWER AFT CORNER INTERNAL BRACKET. REPLACED BRACKET WITH MANUFACTURED BRACKET PE SRM 52-10-02. (M)SDR USAASB03139Ballast · failedCLT - FLT 828 - EN ROUTE FROM IAH-CLT, CAPTAIN REPORTED A STRONG ELECTRICAL ODOR IN THE MID CABIN. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE 'CABIN SERVICE LT O/H LIGHTING' CIRCUIT BREAKER POPPED. CIRCUIT BREAKER WOULD NOT RESET. SUSPECSDR USAASB01275Power Supply · dischargedPHL - MAINTENANCE FOUND SEVERAL EMERGENCY LIGHTS IN THE AFT GALLEY INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. (M)SDR USAASB01099Battery Pack · dischargedALB - MAINTNANCE FOUND THE SEAT MOUNTED EMERGENCY EVACUATION LIGHTS, FROM SEAT ROWS 20 TO 23 INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE AFT GALLEY CEILING, LEFT SIDE. OPS CHECK GOOD. (M)SDR USAASB01050Arm · out of rigPHL - FLT 1484 - ON CLIMB-OUT FROM PHL, EN ROUTE TO BTV, THE AIRCRAFT WOULD NOT PRESSURIZE. THE FORWARD MAIN ENTRY DOOR DID NOT SEAL PROPERLY. CREW NOTED THAT NO DOOR INDICATION WAS GIVEN BEFORE TAKEOFF. FLIGHT RETURNED TO FIELD AT PHL AND LANDED WITHOUT FUSDR USAA002189Skin · crackedPIT - FOUND LEFT ELEVATOR .625 INCH LONG CRACK, TOP SIDE SKIN AT CORNER OF TAB CUT OUT ELEV STATION 123. REMOVED CRACK, TAPER SANDER BACK THEN REPLACED LAYER PLUS 2 EXTRAS EPR SRM 55-20-01, AND 51-70-17 AND EA. (M)SDR USAA002106Crossbeam · wornPIT - FOUND ENGINE MOUNT CROSSBEAM .015 INCH WEAR, BEARING BORE ON TOP OF MOUNT. OPEN UP BORE .005 ON TOP OF MOUNT. OPEN UP BORE .005 INCH TO INSTALL 2 OVERSIZE BEARINGS PER EA 57451. (M)SDR USAASB99091Valve · failedSTL - FLT2074 - ON CLIMB-OUT FROM CLT, AT APPROX 8,000 FT, THE LT 'NO TRANSFER' LIGHT FOR THE AUX FUEL TANK ILLUMINATED. THE AUX FUEL TANK WAS EMPTY. CONTINUING CLIMB, AT APPROX 15,000 FT, THE LT AND RT MLG RED LIGHTS ILLUMINATED WITH RT L/G GREEN LIGHT ON. SDR USAASB98178Static Line · leakingCLT - FLT 549 - ON CLIMB-OUT FROM CLT, THE CAPTAINS ALTIMETER AND AIRSPEED INDICATOR BECAME INOP. FLIGHT RETURNED TO FIELD AT CLT AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE RESEATED/RERACKED THE NR 1 AIR DATA COMPUTER (P/N 4061100-9SDR USAASB97170Battery Pack · dischargedORD - MAINTENANCE FOUND VARIOUS EMERGENCY EXIT LIGHTING INOP IN THE FORWARD CABIN. MAINTENANCE REMOVED AND REPLACED THE M1132 BATTERY PACK. OPS CHECK GOOD. (M)SDR USAASB97099Circuit Card · failedCLT - FL484 WHILE EN ROUTE AT CRUISE THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. ON DESCENT, THE LIGHT WENT OUT, AT 10,000 FT, THE LIGHT CAME ON AGAIN. CREW TRIED TO PLACE GEAR HANDLE IN THE UP POSITION BUT IT WOULD NOT MOVE FROM THE NEUTRAL POSITION. AS THE FSDR USAASB97084Air Distribution · odorMIA - FL 1888 - DURING CRUISE, AT FL 310, CREW NOTICED SOME SMOKE COMING UP BETWEEN CAPTAINS LEGS. SMOKE STOPPED BUT A PUNGENT ODOR, THE CAPTAIN CHECKED THE CABIN. SAME PUNGENT ODOR WAS PRESENT. CAPTAIN ELECTED TO DIVERT TO MIA AS A PRECAUTION. MAINTENANCESDR USAA960597Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH DIAMETER SPOTS FLOOR BEAM 'T' CAP BS 328 RBL 13, 14, 21, 23, 28, 35, 42, 49. INSTALLED T-CAP CAP SPLICE AND DOUBLERS, REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2.SDR USAA960596Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND 1 INCH DIAMETER SPOTS OF CORROSION TOP OF FLOOR BEAM BS 312 LBL 14 BBL 0 RBL 8. CUT OFF UPPER CHORD RBL 19 TO LBL 33 AND INSTALLED NEW T-CAP. REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LSDR USAA960595Floor Beam · corrosionINT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND CORROSION .25 INCH SPOTS FLOOR BEAM T-CAP BS 344, BL 0 - RBL 8. SPLICED T-CAP INSTALLED FILLER AND DOUBLERS, REPAIRED PER TR 53-10-03. CORROSION TASK NR C53-107-02, CORROSION LEVEL 2. (M)SDR USAA950251Drive Pad · leakingPIT - FLT 1797 - FLIGHT EN ROUTE MCI TO LGA WITH NR 2 ENGINE OIL QUANTITY DECREASING. FLIGHT DIVERTED TO PIT WHERE LANDING WAS WITHOUT FURTHER INCIDENT. MAINTENANCE BAGGED DRAINS AND RAN ENGINE AT TAKEOFF POWER. NO LEAKS FOUND, NO OIL IN INLET OR TAILPIPE. SDR USAA950025Pressurization · malfunctionedORF - FLT 124 - UNABLE TO PRESSURIZE ACFT AFTER TAKEOFF. FLIGHT RETURNED TO ORF WHERE LANDING WAS WITHOUT INCIDENT. MAINTENANCE SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES. OPS CHECK NORMAL. SWAPPED FWD AND AFT ZONE TEMP CONTROL BOXES. OPS CHECK NORMAL.
Back to N436US, cancelled Feb 2, 2007